Device and method for checking an aircraft landing gear shock absorber
First Claim
1. A method of checking whether a characteristic of the gas in an aircraft landing gear oleo is acceptable or not for an aircraft which is at rest, the oleo comprising an inner sliding tube having a known diameter and an outer covering in which the inner sliding tube slides, the exposed region of inner sliding tube being indicative of the amount of extension of the oleo, the method comprising the following steps:
- capturing an image which depends on the amount of extension of the oleo with a hand-held electronic device, the image comprising said exposed region,measuring a width and height of the part of the image that defines the exposed region with the hand-held electronic device,deriving the amount of extension of the oleo with the hand-held device from the measured width and height of the part of the image that defines the exposed region and from the known value of the diameter of the inner sliding tube,obtaining an indication of the expected value of the characteristic of the gas in the oleo with the hand-held device from the amount of extension of the oleo,outputting with the hand-held electronic device an output in dependence on that indication of the expected value, providing a measure of the pressure in the landing gear obtained by other means, and generating an expected pressure from the measure of extension of the oleo and comparing the expected pressure to the pressure in the landing gear obtained by other means.
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Accused Products
Abstract
An electronic device checks the pressure of an aircraft landing gear oleo by means of a camera capturing and processing an image of the oleo. An image recognition module processes the oleo image to extract a measure of the amount of extension of the oleo. This measure is then processed together with a measure of oleo temperature to calculate a pressure value representative of the expected pressure of the gas within the oleo, which can then be compared with another measurement of oleo pressure to determine whether the two are consistent or whether the oleo might be under- or over-filled with gas. The electronic device may be in the form of a hand-held smart phone or tablet device appropriately programmed with software.
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Citations
17 Claims
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1. A method of checking whether a characteristic of the gas in an aircraft landing gear oleo is acceptable or not for an aircraft which is at rest, the oleo comprising an inner sliding tube having a known diameter and an outer covering in which the inner sliding tube slides, the exposed region of inner sliding tube being indicative of the amount of extension of the oleo, the method comprising the following steps:
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capturing an image which depends on the amount of extension of the oleo with a hand-held electronic device, the image comprising said exposed region, measuring a width and height of the part of the image that defines the exposed region with the hand-held electronic device, deriving the amount of extension of the oleo with the hand-held device from the measured width and height of the part of the image that defines the exposed region and from the known value of the diameter of the inner sliding tube, obtaining an indication of the expected value of the characteristic of the gas in the oleo with the hand-held device from the amount of extension of the oleo, outputting with the hand-held electronic device an output in dependence on that indication of the expected value, providing a measure of the pressure in the landing gear obtained by other means, and generating an expected pressure from the measure of extension of the oleo and comparing the expected pressure to the pressure in the landing gear obtained by other means. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10)
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11. A method of checking whether a characteristic of the gas in an aircraft landing gear oleo is acceptable or not for an aircraft which is at rest, the oleo comprising an inner sliding tube having a known diameter and an outer covering in which the inner sliding tube slides, the exposed region of inner sliding tube being indicative of the amount of extension of the oleo, the method comprising the following steps:
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capturing an image which depends on the amount of extension of the oleo with a hand-held electronic device, the image comprising said exposed region, measuring a width and height of the part of the image that defines the exposed region with the hand-held electronic device, deriving the amount of extension of the oleo with the hand-held device from the measured width and height of the part of the image that defines the exposed region and from the known value of the diameter of the inner sliding tube, obtaining an indication of the expected value of the characteristic of the gas in the oleo with the hand-held device from the amount of extension of the oleo, outputting with the hand-held electronic device an output in dependence on that indication of the expected value, inputting a temperature value representative of the temperature of the oleo, generating an expected pressure value from the inputted temperature value and the measure of the extension of the oleo, and comparing the expected pressure value with a measure of the pressure in the landing gear oleo obtained via other means.
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12. A method of checking whether a characteristic of the gas in an aircraft landing gear oleo is acceptable or not for an aircraft which is at rest, the oleo comprising an inner sliding tube having a known diameter and an outer covering in which the inner sliding tube slides, the exposed region of inner sliding tube being indicative of the amount of extension of the oleo, the method comprising the following steps:
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capturing an image which depends on the amount of extension of the oleo with a hand-held electronic device, the image comprising said exposed region, measuring a width and height of the part of the image that defines the exposed region with the hand-held electronic device, deriving the amount of extension of the oleo with the hand-held device from the measured width and height of the part of the image that defines the exposed region and from the known value of the diameter of the inner sliding tube, obtaining an indication of the expected value of the characteristic of the gas in the oleo with the hand-held device from the amount of extension of the oleo, outputting with the hand-held electronic device an output in dependence on that indication of the expected value, inputting a temperature value representative of the temperature of the oleo, generating an expected oleo extension from the inputted temperature value and a measure of the pressure in the landing gear obtained by other means, and wherein the expected oleo extension and the measured oleo extension are compared, and electronically producing an output dependent on said comparison.
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13. A method of checking whether a characteristic of the gas in an aircraft landing gear oleo is acceptable or not for an aircraft which is at rest, the oleo comprising an inner sliding tube having a known diameter and an outer covering in which the inner sliding tube slides, the exposed region of inner sliding tube being indicative of the amount of extension of the oleo, the method comprising the following steps:
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capturing an image which depends on the amount of extension of the oleo with a hand-held electronic device, the image comprising said exposed region, measuring a width and height of the part of the image that defines the exposed region with the hand-held electronic device, deriving the amount of extension of the oleo with the hand-held device from the measured width and height of the part of the image that defines the exposed region and from the known value of the diameter of the inner sliding tube, obtaining an indication of the expected value of the characteristic of the gas in the oleo with the hand-held device from the amount of extension of the oleo, outputting with the hand-held electronic device an output in dependence on that indication of the expected value, providing a measure of the pressure in the landing gear obtained by other means, and generating an expected extension value of the oleo from the measure of the pressure in the landing gear obtained by other means, and comparing the expected oleo extension to the measure of the extension of the oleo. - View Dependent Claims (14, 15, 16, 17)
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Specification